Acta Aerodynanica Sinica (Selected Articles),
Abstract
Titles include: Advances in the Study of Separated Flows; Problems in Discrete Vortex Numerical Modelling of Vortex Motion behind a Circular Cylinder; Calculation of Slender Delta Wing with Leading-edge Separation by Quasi-vortex-lattice Method; Calculation of Flow around Thick Wing with Separation Vortices; Split Coefficient Matrix Difference Method for Supersonic Three-dimensional Flow; Some Characteristics of the FLIC Method and Its Application to Calculation of Pitot Pressure of Dusty-Gas Shock Tube Flow; Experimental Investigation of Flap Turbulent Heat Transfer and Pressure Characteristics in Hypersonic Flow; Laser Doppler Anemometer Measurements for Leading Edge Vortex Core Velocity of a Strake-wing; Experimental Research of Boundary Layer Control Technique for Low Speed Multi-component Airfoils; A Simpler Implicit Method to Solve N-S Equation; Numerical Calculation of Separation Flow over Severely Indented Blunt Body; Implicit Technique for Calculating Separated Base Flow; Computation of Compressible Turbulent Separated Boundary Layer; Inverse Boundary Layer Method for Separated Flow; Wall Lift Interference Corrections in Ground Effect Testing. (Translations; China; Chinese language)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 05, 1985
- Accession Number
- ADA162993
Entities
People
- Fenggan Zhuang
- Guocan Ling
- Hanxin Zhang
- Peiye Zhu
- Shauwen Xiung
Organizations
- National Air and Space Intelligence Center